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NASA Technical Reports Server (NTRS) 19930087692: Investigation of a 10-stage Subsonic Axial-flow Research Compressor V : Effect of Reducing Inlet-guide-vane Turning on Over-all and Inlet-stage Performance

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NASA Technical Reports Server (NTRS) 19930087692: Investigation of a 10-stage Subsonic Axial-flow Research Compressor V : Effect of Reducing Inlet-guide-vane Turning on Over-all and Inlet-stage Performance

by
NASA Technical Reports Server (NTRS)

Publication date
Topics
NASA Technical Reports Server (NTRS),
Collection
NASA_NTRS_Archive; additional_collections
Language
English
Addeddate
2016-03-24 14:48:24
Identifier
NASA_NTRS_Archive_19930087692
Identifier-ark
ark:/13960/t59d1bb60
Ocr
ABBYY FineReader 11.0
Pages
40
Ppi
600
Year
1954

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